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Accidents · NTSB ERA09LA187 · Final report

Amateur-built Sonerai-II accident near Leonardtown, Maryland, March 6, 2009

On March 6, 2009 at about 5:44 pm local time, a amateur-built Sonerai-II, registered N28MD, was substantially damaged in an accident during initial climb near Leonardtown, Maryland (St. Mary'S County Regional airport). It was a personal flight under general aviation rules (Part 91). 1 person had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's continued operation of the airplane with a known mechanical deficiency. Contributing to the accident was the improper installation of the electronic ignition system.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 6, 2009 · about 5:44 pm local time
Place
Leonardtown, Maryland · St. Mary'S County Regional · map
Type
Accident
Injuries
1 person had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Amateur-built Sonerai-II
Registration
N28MD · registry record · serial 141
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

According to the pilot/owner of the amateur-built airplane, after performing an engine check, he noticed the sole engine-driven magneto was not operating normally. However, since he had an electronic ignition system, he felt it would be acceptable to remain in the traffic pattern at the airport. While climbing through approximately 400 feet on his sixth takeoff, the engine started to lose power. The pilot/owner manipulated the throttle; however, the engine failed to respond. During the off-airport forced landing, the airplane impacted a tree with the outboard portion of the right wing. Following the recovery of the wreckage, the No. 2 cylinder exhaust pipe was observed detached and the exhaust outlet was in close proximity to the electronic ignition and coil that provided power to the cylinders. Additionally, the fuse to the ignition system was also found blown. After replacing the fuse, the engine operated normally utilizing the electronic ignition system. Manufacturer guidance indicates that the installation of the electronic ignition system should be on the accessory gear box next to the engine driven magneto, in order to prevent excessive temperatures to the coils. In the accident airplane, the electronic ignition system was mounted on the firewall, near the No. 2 exhaust.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Powerplant sys/comp malf/fail during taxi (to runway)
  2. Loss of engine power (partial) during initial climb defining event
  3. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • cause Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • factor Aircraft › Aircraft power plant › Ignition system › Magneto/distributor › Inoperative
  • factor Aircraft › Aircraft power plant › Ignition system › Ignition power supply › Capability exceeded
  • Environmental issues › Physical environment › Object/animal/substance › Tree(s) › Contributed to outcome
  • factor Personnel issues › Task performance › Maintenance › Installation › Owner/builder

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 609 hours in all; 180 in this make and model; 10 in the last 90 days; 2 in the last 30 days; 561 as pilot in command
  • Last flight review: June 15, 2007
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: rear
  • Injury: minor injuries

The aircraft

  • Airframe total time: 180 hours
  • Last inspection: condition inspection, August 13, 2008; 37 hours since
  • Maximum gross weight: 950 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Volkswagon/Great Plains VW 2180 (piston); 0 hours total

The flight

  • Departed from: 2W6 Leonardtown MD at 5:00 pm
  • Destination: 2W6 Leonardtown MD
  • Flight plan: none
  • Runway 29, 4,150 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 220° at 12 knots, gusting 16
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 55°F (13°C), dew point 36°F (2°C)
  • Altimeter: 30.12 inHg
  • Observation at 5:52 pm from 2W6, 2 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Other NTSB records under N28MD the same tail number, which may have belonged to a different aircraft at the time

2025-12-12CEN26LA060 · accident near Cresson, TX · substantial damage · serious injuries

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.